- Owner type
- Co-owned, fractional ownership
- Serial number
- 680A0044
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 1, 2016
- Certificate issued
- October 8, 2026
- Expires
- October 31, 2033
- Mode S code
- A65560
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 3
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2018 | 1 |
|---|---|
| 2023 | 1 |
| 2026 | 1 |
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N507QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Textron 680A aircraft
FAA incident reports
No FAA accident or incident reports matched to N507QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Textron 680A aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026022707028Pressure Switch · illuminatedWHEN SELECTING THE CROSSFEED FROM L TANK TO RIGHT ENGINE, RECEIVED AMBER CAS MESSAGE: FUEL BOOST PUMP R. FOLLOWED THE QRH. MESSAGE DID EXTINGUISH. THIS CONDITION HAS HAD A PREVIOUS HISTORY OF SUCH. SENT ARES TO CESSNA TEAM680 FOR EVALUATION. FOUND LH FUEL LOWSDR DXTA2025122606267Cartridge · unknownIN CRUISE FLIGHT SELECTED FUEL TRANSFER FROM LEFT TANK TO RIGHT TANK RIGHT BOOT PUMP CAS MESSAGE ELIMINATED COMPLETED CHECKLIST. EVERYTHING RETURNED TO NORMAL TRIED TO TRANSFER AGAIN THIS TIME RECEIVED A LOW PRESSURE WARNING WITH NO BOOT PUMP. SYSTEM WORKED FISDR DXTA2025121506099Check Valve · defectiveIN LEVEL FLIGHT WE SELECTED THE FUEL CROSSFEED SELECTOR TO THE LEFT TANK THE WHITE LEFT FUEL BOOST AS IT SHOULD BUT A FEW SECOND LATER THE RIGHT AMBER BOOST PUMP CAS MESSAGE COMES ON. WHEN YOU SELECT THE CROSSFEED TO OFF AND FOLLOW THE CHECKLIST YOU CAN GET THSDR DXTA2025043003268Hydraulic System · leakingDURING DESCENT WE RECEIVED THE HYD VOLUME LOW CAS MESSAGE. VOLUME INDICATED 120 CU IN. WE FOLLOWED THE QRH PROCEDURE AND UNLOADED THE ENGINE DRIVEN PUMPS. QUANTITY SETTLED AT 140-160 AFTER UNLOADING PUMPS. LANDED USING QRH PROCEDURE AND DID USE THE EMERGENCSDR 2025FA0000111Skin · debondedDEBONDING OF LH AND RH WING UPPER SKIN ASSEMBLY STRINGER ENDS: ACCOMPLISHED INJECTION OF ADHESIVE INTO DEBONDED AREA AND ADDED FASTENERS TO THE END OF THE AFFECTED STRINGERS. VERIFIED NO CRACK INDICATIONS EXIST IN THE UPPER WING SKIN IN THE DEFECT AREAS AND RESDR DXTA2024012310697Squat Switch · faultedUPON GEAR RETRACTION AFTER TAKEOFF RECEIVED A GEAR DISAGREE RT & AMBER DN IND ON RT MLG & NOSE & LT MLG RETRACTED NORMAL. RAN ABNORMAL CHECKLIST, EXTENDED GEAR HANDLE AND RECEIVED 3 GREEN DWN. LANDED WITHOUT ISSUE. REMOVED RT MLG DOWN LOCK SWITCH & CLEANED SESDR DXTA2023103099190Unknown · unknownUNABLE TO MOVE HANDLE TO THE CLOSED POSITION. FOUND ONE AFT CABIN DOOR PIN BOUND UP AND NOT LETTING THE DOOR HANDLE MOVE. REMOVED CABIN DOOR STEPS. FREED UP DOOR PIN AND LUBED IAW CE-680A AMM 12-20-40. HANDLE IS NOW MOVING NORMALLY. REINSTALLED CABIN STEPS ISDR DXTA2023091194980Unknown · unknownEMERGENCY LIGHTING: WITH BOTH SHIP BATTERIES CONNECTED, AND BATTERY SWITCHES OFF, WHEN GOING TO ON FOR EMER LIGHTS, NO EMERGENCY LIGHTS COME ON AT ALL. //SIGNOFF// EMERGENCY LIGHTING: WITH BOTH SHIP BATTERIES CONNECTED, AND BATTERY SWITCHES OFF, WHEN GOING TO SDR DXTA2022072066350Screw · shearedAFTER FRA I SWITCHED THE YAW DAMPER ON. THE FO THAT WAS PF SAID HE FELT THE RUDDERS MOVE STRANGELY AND WE RECEIVED AN AP YD FAIL MESSAGE. // SIGNOFF// PERFORMED LITEF LCR-100 HYBRID NAVIGATOR OPS CHECK. NO FAULTS FOUND. NOTIFIED MCC AND THEY ELECTED TO CHANGE SDR DXTA2021121353390None · noneLAV EMERG LIGHT: LAV UNDERSEAT LIGHT INOP // SIGNOFF// REMOVED PANEL UNDER LAV SEAT AND NOTED CANNON PLUG DISCONNECTED. RECONNECTED CANNON PLUG AND COMPLIED WITH SATISFACTORY OPS CHECKS AT THIS TIME PER CE-680A MM 33-50-00.SDR 2021FA0000268Skin · corrodedCORROSION ON LH VERTICAL STAB SKIN T/E BETWEEN MIDDLE AND LOWER HINGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO DQ31657 DATED SEPTEMBER 26, 2021.SDR DXTA201806041034Contactor · faultedDURING CRUISE, AT FL430, RECEIVED A RIGHT DC EMERGENCY BUSS AMBER CAS MESSAGE. FOLLOWED CHECKLISTS AND LANDED WITHOUT INCIDENT. REMOVED THE FAULITY RT BUSS CONTACTOR KZ014. OPS CHECKED GOOD IAW AMM 24-60-10-2, AND 24-60-10-5.
Reports on N507QS not matched to an aircraft · 8
They name N507QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2012031504921Warning Message · false activationLEFT ENGINE DATA MISCOMPARE. HIGH OIL TEMP CAS MESSAGES. PRECAUTIONARY SHUTDOWN. COULD NOT DUPLICATE DISCREPANCY.SDR 2007FA0001015Connector · crackedBACK SHELL IS BROKEN/CRACKED AND SEPARATED FROM CONNECTOR PLUG ASSY. POSSIBLE CAUSE IS WIRE BUNDLE TO CONNECTOR PLUG STRESSES AND PULLING ON BACK SHELL. BACK SHELL IS MADE ON PLASTIC NOT METAL. IF BACK SHELL WAS MADE OF METAL IT WOULD HOLD UP AS A STRAIN RELSDR 625060606AAdapter · corrodedLEFT MAIN LANDING GEAR AXLE ADAPTER HAS CORROSION AND PITTING.
STCs that may be installed · 16
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Textron 680A
STC ST04765NYUnprepared (Grass/Sod) Runway OperationsSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST12344IBReplacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher